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Journal Article

Approach for an Integrated Multi-Domain Aircraft Energy Model

2008-11-11
2008-01-2917
In recent years, More-Electric and All-Electric Architectures are being adopted extensively for next generation of aircraft. In this new architecture, many systems rely primarily on the use of electrical energy. Hence, there is a significant increase in the demand of electrical energy that is managed by the electric power system of the aircraft. A significant increase in demand of electrical power is also observed during recent years of aircraft development. In the More-Electric Architecture, aircraft systems are heavily dependent on electric energy. This fact results in higher extraction of mechanical power from the engine via power take off shafts as opposed to energy extraction via bleed air. The balance of extracted energies has shifted from pneumatic extraction to mechanical extraction and conversion into electrical power. The transition to the use of increased levels of electrical power leads to increased complexity and criticality of the electrical system of the aircraft.
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